Transient Dynamic Response of the Aero-Engine Dual-Rotor System Under the Blades Loss Load
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_240
Reference12 articles.
1. Raffa FA, Vatta V (1996) The dynamic stiffness method for linear rotor-bearing system. ASME J Vib Acoust 118(7):332–339
2. Grapis O et al (2006) Overcritical high-speed rotor systems full annular rub and accident. J Sound Vib 290:910–927
3. Sinha SK (2013) Rotor dynamic analysis of asymmetric turbofan rotor due to fan blade-loss event with contact-impact rub loads. J Sound Vib 332(9):2253–2283
4. Ming Z, Ming D, Changfu L (2016) Structural Analysis of Aero Engine. Northwestern Polytechnical University Press, Xian
5. Guang C (2014) Structural Design Analysis of Aero Engine. Beihang University Press, Beijing
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